A shock wave detection system includes a light beam emitter, a light beam receiver and an analysis unit. The light beam emitter emits a light beam oblique to a direction of an air flow through which a shock wave may propagate. The light beam receiver receives the light beam that has passed through the air flow. The analysis unit is configured to detect a presence and a position of the shock wave based on a change in a receiving position of the light beam by the light beam receiver.


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    Title :

    SHOCK WAVE DETECTION SYSTEM, METHOD OF DETECTING SHOCK WAVE AND AIRCRAFT


    Contributors:
    SATO RYOSUKE (author) / TAKAYA RYOTA (author)

    Publication date :

    2024-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01H MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES , Messen von mechanischen Schwingungen oder Ultraschall-, Schall- oder Infraschallwellen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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